Airbus Helicopters H225 vs Piaggio Avanti Evo vs Sikorsky S 92
The Airbus H225 and Sikorsky S‑92 are large, twin‑engine helicopters typically used for offshore transport, SAR, and utility missions, while the Piaggio Avanti EVO is a twin‑turboprop fixed‑wing business aircraft optimized for fast point‑to‑point travel on runways. In range, the Avanti EVO generally offers the longest legs, commonly around 1,500–1,800 nautical miles depending on payload and reserves, whereas the H225 and S‑92 are usually in the several-hundred‑nautical‑mile class (often roughly 450–550 nautical miles), with exact figures varying by configuration and mission profile. For passenger capacity, both helicopters can be configured to carry more people than the Avanti: the S‑92 is often arranged for about 19 passengers in transport layouts, and the H225 is commonly in a similar high‑teens to around 19‑seat class. The Avanti EVO typically seats fewer, usually 7–9 passengers in executive configuration. Overall, Avanti EVO leads on range and cruise efficiency, while H225 and S‑92 lead on vertical access and higher passenger lift in rotorcraft roles.
| Spec | AIRBUS H225 | Piaggio Avanti EVO | Sikorsky S-92 |
|---|---|---|---|
| Summary | |||
| Cockpit | 2 | 2 | 2 |
| DOC / nm | $ 20.87 | — | $ 19.79 |
| Min Crew | 2 | 1 | 2 |
| Total Seats | 21 | 8 | 21 |
| Flight Rules | IFR | IFR | IFR |
| Manufacturer | Airbus Helicopters | Piaggio | Sikorsky |
| Aircraft Name | H225 | Avanti EVO | S-92 |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 454 | 1530 | 439 |
| DOC / nm / Seat | $ 0.99 | — | $ 0.94 |
| Max Cabin Seats | 28 | 7 | 19 |
| OEM Verification | Un-Verified | Un-Verified | Un-Verified |
| Useful Load (lbs) | 11929 | 3775 | 7417 |
| Standard Cabin Seats | 19 | 6 | 19 |
| Direct Operating Cost | $ 2,963 | — | $ 3,068 |
| Flight Deck (Base Spec) | EFIS | Rockwell Collins Pro Line 21 | EFIS |
| Max Cruise Speed (ktas) | 142 | 400 | 155 |
| Base Aircraft Price (USD) | $ 29,500,000 | $ 7,695,000 | $30,650,000 |
| Cabin | |||
| Cockpit | 2 | 2 | 2 |
| Min Crew | 2 | 1 | 2 |
| Total Seats | 21 | 8 | 21 |
| Max Cabin Seats | 28 | 7 | 19 |
| Standard Cabin Seats | 19 | 6 | 19 |
| Lavatory | — | No | — |
| Cabin Pressure (psi) | — | 9 | — |
| Galley / Refreshment | — | No | — |
| SL Cabin Altitude (ft) | — | 24000 | — |
| Max Cabin Altitude (ft) | — | 6600 | — |
| Engine | |||
| FADEC | Yes | Yes | Yes |
| Model | Makila 2A1 | PT6A–66B | CT7-8A |
| Fuel Type | JetFuel | — | JetFuel |
| TBO (hrs) | 3500 | 3600 | 4000 |
| Horsepower | 2100 | 850 | 2520 |
| No. of Engines | 2 | 2 | 1 |
| Fuel Capacity (gal) | 684 | — | 760 |
| Flat Rating | — | ISA + 28 | — |
| Fuel Burn (gph) | — | 100 | — |
| Dimensions | |||
| Length (ft) | 63.4 | 47.3 | — |
| Overall Height (ft) | 16.3 | 13.1 | 17.8 |
| Rotor Diameter (ft) | 53.2 | — | — |
| Cabin Volume (cu. ft) | 547 | — | 775 |
| Wingspan (ft) | — | 47.1 | — |
| Cabin Width (ft) | — | 6.1 | — |
| Cabin Height (ft) | — | 5.8 | — |
| Cabin Length (ft) | — | 14.9 | — |
| Cabin Width - Floor (ft) | — | 3.5 | — |
| Baggage Volume Int. (cu. ft) | — | 35.2 | — |
| Baggage Volume Ext. (cu. ft) | — | — | 140 |